TextPartly OCR
Some pages are OCR from a scan. OCR can misread letters and numbers.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '1e6830ab7d4a8c7c85d0dc6e36117b7a77c0671b5050b8a55776f072e99b54b8' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '1e6830ab7d4a8c7c85d0dc6e36117b7a77c0671b5050b8a55776f072e99b54b8' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
FALCON 2000 No 441 JUNE 20, 2017
ATA 30-13
ICE AND RAIN PROTECTION
WING ANTI-ICING DISTRIBUTION
INSPECTION OF THE WING ANTI-ICING BALL JOINT
FALCON SERVICE BULLETIN Copyright © 2017 by Dassault Aviation All rights reserved. No part of this work may be reproduced or copied in any form or by any means without written permission of Dassault Aviation.
ICE AND RAIN PROTECTION
WING ANTI-ICING DISTRIBUTION
INSPECTION OF THE WING ANTI-ICING BALL JOINT Initial issuance June 20, 2017 List of effective pages :
1 to 15 FALCON 2000 F2000 -441 F2000 -30-13
ICE AND RAIN PROTECTION
WING ANTI-ICING DISTRIBUTION
INSPECTION OF THE WING ANTI-ICING BALL JOINT
1. PLANNING INFORMATION A. EFFECTIVITY This Service Bulletin is applicable to FALCON 2000 aircraft with serial numbers 1 through 231.
B. REASON Some FALCON 2000 operators reported internal object debris in the wing anti-icing ducting.
Depending on the size and location of the debris, the wing leading edges/slats might be supplied with improper anti-ice airflow.
Investigation revealed that debris originated from the flow guide of a ball joint located downstream of the wing anti-ice valve.
The purpose of this Service Bulletin is to check the integrity of the ball joint flow guide and take corrective actions in case of damage.
C. DESCRIPTION The operation consists in inspecting the wing anti-icing ball joint, and depending on the inspection results:
• replacing the ball joint (and the pipe attached to it) in case of damage to the flow guide and/or,
• performing a borescope inspection of all wing anti-icing pipes in case of damage and release of debris from the flow guide.
D. COMPLIANCE If you choose to comply with this Service Bulletin, accomplishment is to be performed during the next “Z” inspection.
E. APPROVAL The technical content of this document is approved under the authority of DOA nr. EASA.21J.051.
F. LABOR Estimated labor-hours:
• Refer to Service Bulletin Commercial Summary.
• An engine run-up is necessary to perform the leak check after wing anti-icing valve installation.
NOTE: These labor-hours only concern the work described in this Service Bulletin and do not include other maintenance work that may be performed on this occasion.
G. MATERIAL - PRICE AND AVAILABILITY The modification kit may be obtained from either address listed below:
Western hemisphere: DASSAULT FALCON JET CORP.
FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 1 / 15 DASSAULT AVIATION Proprietary Data
SPARES DISTRIBUTION CENTER 200 RISER ROAD LITTLE FERRY, NJ 07643 U.S.A.
Telephone:
• CANADA and U.S.A.: 1-800-800-4036
• MEXICO: 001-800-800-4036
• Other countries: 1-201-541-4809 Fax:
• CANADA and U.S.A.: 1-800-800-4817
• MEXICO: 001-800-800-4817
• Other countries: 1-201-440-7021 Other continents: DASSAULT AVIATION Falcon Spares BOITE POSTALE N°101
AEROPORT DU BOURGET 93350 - LE BOURGET Cedex (FRANCE) Please contact your Dassault Aviation Account Representative Telephone: 33 (0)1.48.35.56.78 Fax: 33 (0)1.48.35.56.00 E/H dafsorder@dassault-aviation.com Price and availability on request.
H. TOOLING - PRICE AND AVAILABILITY Normal maintenance tooling.
Borescope kit with a 3 m-length (10 ft).
Plexiglas spatula.
I. WEIGHT AND BALANCE Change in weight: None.
Change in balance with respect to 25% MAC: None.
J. ELECTRICAL LOAD ANALYSIS None K. REFERENCES Aircraft Maintenance Manual:
• GENERAL MAINTENANCE AND SAFETY PRECAUTIONS (Refer to TASK 20-00-00-910-801)
• REMOVAL / INSTALLATION OF WIGGINS W991 COUPLINGS (Refer to TASK 20-41-00-900-801)
• REMOVAL / INSTALLATION OF FLEXINOX CLAMPS (Refer to TASK 20-41-00-900-809)
• LEAK CHECK OF THE WING ANTI-ICING SYSTEM (Refer to TASK 30-10-00-790-801) FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 2 / 15 DASSAULT AVIATION Proprietary Data
• REMOVAL / INSTALLATION OF THE SLAT TELESCOPIC DUCTS (Refer to TASK 30-11-09-900-801)
• REPLACEMENT OF THE PICCOLO TUBES (Refer to TASK 30-11-11-960-801)
• REMOVAL / INSTALLATION OF THE WING ANTI-ICING VALVE (Refer to TASK 30-12-01-900-801)
• REMOVAL / INSTALLATION OF THE BRAKE HEATING VALVES (Refer to TASK 30-90-01-900-801)
• REMOVAL / INSTALLATION OF THE FUSELAGE FAIRINGS (Refer to TASK 53-60-01-900-801) L. OTHER PUBLICATIONS AFFECTED The following publications will be revised at a later date to account for the changes introduced by this Service Bulletin:
• Maintenance Manual.
• Illustrated parts Catalog.
FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 3 / 15 DASSAULT AVIATION Proprietary Data
2. ACCOMPLISHMENT INSTRUCTIONS A. PRELIMINARY STEPS
(1) The aircraft must be in the maintenance configuration (Refer to TASK 20-00-00-910-801).
(2) Remove wing anti-icing valve ( 20DL) (Refer to TASK 30-12-01-900-801 ) to gain access to the ball joint (fig. 1).
B. INSPECTION OF THE BALL JOINT Refer to fig. 2
(1) Check for absence of cracks and loss of material on the internal parts of the ball joint (flow guide):
(a) If no cracks or loss of material are found, no further action is required, install wing anti-icing valve (20DL) (Refer to TASK 30-12-01-900-801).
(b) If any cracks are found:
• Fill out the inspection report ( fig. 6) taking picture of the damage.
• Fill out e-form under the Falcon Portal NOTE: For aircraft without access to Falcon Portal, send the inspection report to CommandCenter@dassault-aviation.com
• Replace the ball joint with its pipe (refer to paragraph 2.C.).
(c) If loss of material are found:
• Search for the fragments present in the wing anti-icing pipes.
• Perform a borescope inspection of all the wing anti-icing pipes (refer to paragraphe
2.D.).
• Remove all the fragments from the wing anti-icing pipes.
• Fill out the inspection report ( fig. 6) taking pictures of the damage.
• Fill out e-form under the Falcon Portal NOTE: For aircraft without access to Falcon Portal, send the inspection report to CommandCenter@dassault-aviation.com
• Replace the ball joint with its pipe (refer to paragraph 2.C.).
C. REPLACEMENT OF THE BALL JOINT NOTE: The ball joint is part of pipe P/N F2MA724561A (g-fig. 1) and cannot be replaced separatly.
(1) Remove forward servicing compartment floor panel ( 322AZ) and forward servicing compartment floor panel (322BZ).
(2) Disconnect the exchanger air intake pipe:
(a) Loosen the nut (a-fig. 1).
(b) Disconnect the pipe (b-fig. 1 ).
(3) Remove the attaching plate:
FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 4 / 15 DASSAULT AVIATION Proprietary Data
(a) Remove the two screws ( c-fig. 1).
(b) Remove the clamp and extrusion ( d-fig. 1).
(4) Disconnect the other end of the pipe as follows:
(a) Remove the sealant CAF4 on each end of the insulation (e-fig. 1) with a Plexiglas spatula.
(b) Remove the insulation ( e-fig. 1).
(c) Remove the union ( f-fig. 1).
(d) Remove and discard the pipe ( g-fig. 1).
(5) Put a new pipe P/N F2MA724561A in position ( g-fig. 1).
(6) Connect the end of the pipe as follows:
(a) Install the union ( f-fig. 1).
(b) Install the insulation ( e-fig. 1).
(c) Apply sealant CAF4 at each end of the insulation (e-fig. 1).
(7) Install the attaching plate:
(a) Install the extrusion and clamp ( d-fig. 1).
(b) Install the two screws ( c-fig. 1).
(c) Tighten the screws ( c-fig. 1).
(8) Connect the exchanger air intake pipe:
(a) Put the pipe in position ( b-fig. 1).
(b) Tighten the nut ( a-fig. 1).
(9) Install wing anti-icing valve ( 20DL) (Refer to TASK 30-12-01-900-801).
(10) Install forward servicing compartment floor panel (322AZ) and forward servicing compartment floor panel (322BZ).
D. INSPECTION OF THE ANTI-ICING PIPES
(1) Inspection of the wing anti-icing pipe ( j-fig. 4):
(a) Remove the following access doors, fairings and panels:
• ( 251CL), (143BL), (261AL) and (512BT) (Refer to TASK 53-60-01-900-801).
• ( 252CR), (144BR), (262AR) and (612BT) (Refer to TASK 53-60-01-900-801).
(b) Remove the pipe ( r-fig. 4):
• Remove the two clamps (k-fig. 4 ) and the two seals (l-fig. 4 ) (Refer to TASK 20-41-00-900-801).
• Remove the two clamps (m-fig. 4 ) and the two seals (n-fig. 4 ) (Refer to TASK 20-41-00-900-801).
• Remove the extrusion ( o-fig. 4), the two clamps (p-fig. 4) and the bushing (q-fig. 4).
• Remove the pipe ( r-fig. 4).
(c) Inspect the wing anti-icing pipe ( j-fig. 4):
• Insert a borescope into the pipe.
• Check for damage or debris in the pipe.
FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 5 / 15 DASSAULT AVIATION Proprietary Data
(2) Inpection of inboard fixed leading edge tubes:
(a) Inspect the inboard fixed leading edge tube:
• Insert the borescope into the pipe ( s-fig. 4).
• Check for damage, nicks or debris.
(3) Inspection of the outboard piccolo tubes:
(a) Remove:
• The four screws ( aa-fig. 3) and washers (ab-fig. 3).
• The ball joint housing ( ac-fig. 3) from the slat.
• Discard O-ring ( ad-fig. 3).
(b) Manually set the telescopic duct to the retracted position.
(c) Inspect telescopic ducts ( 30DL)/(40DL):
• Insert the borescope in the sliding duct ( h-fig. 3).
• Check for damage, nicks or debris.
(d) Remove the outboard piccolo tubes (Refer to TASK 30-11-11-960-801).
(e) Slowly move the piccolo tube into a vertical position, with the telescopic duct hole at the bottom.
(f) Check for debris inside the piccolo tube.
(g) Install the outboard piccolo tubes (Refer to TASK 30-11-11-960-801).
(h) Install the new O-ring P/N R04095X262A50D7 (ad-fig. 3), coated with lubricant for seals in contact with hot air or liquid soap, on the ball-joint housing end-fitting (slat side) (ac-fig.
3).
(i) Position the telescopic duct by moving it upwards.
(j) Install the ball joint housing ( ac-fig. 3) on wing side as follows:
• Manually set the telescopic duct in the extended position.
• Position the ball-joint housing (ac-fig. 3), after applying a coat of high temperature sealant to the base.
• Check that the O-ring ( ad-fig. 3) engages the end-fitting correctly.
• Install the four washers ( ab-fig. 3) and screws (aa-fig. 3).
• Tighten the four screws ( aa-fig. 3).
(4) Inspection of the fuselage anti-icing pipes:
(a) Inspect the pipe ( r-fig. 4):
• Insert the borescope into the pipe.
• Check for damage, nicks or debris.
(b) Inspect the upstream pipe:
• Insert the borescope into the pipe ( t-fig. 4).
• Check for damage, nicks or debris.
(c) Install the pipe:
• Put the pipe ( r-fig. 4) in position.
• Install the bushing ( q-fig. 4), the two clamps (p-fig. 4) and the extrusion (o-fig. 4).
FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 6 / 15 DASSAULT AVIATION Proprietary Data
• Install the two O-rings (l-fig. 4 ) and the two clamps (k-fig. 4 ) (Refer to TASK 20-41-00-900-801).
• Install the two O-rings (n-fig. 4 ) and the two clamps (m-fig. 4 ) (Refer to TASK 20-41-00-900-801).
(5) Inspection of the anti-icing pipes at frame 26:
(a) Gain access to the anti-icing pipe at frame 26:
• Remove forward servicing compartment floor panel (322AZ) and forward servicing compartment floor panel (322BZ).
(b) Disconnect the ball joint pipe as follow:
• Disconnect the exchanger air intake pipe:
• Loosen the nut ( a-fig. 1).
• Disconnect the pipe ( b-fig. 1).
• Remove the attaching plate:
• Remove the two screws ( c-fig. 1).
• Remove the clamp and extrusion ( d-fig. 1) (Refer to TASK 20-41-00-900-809).
• Disconnect the end of the pipe:
• Remove the sealant CAF4 on each end of the insulation (100DL-fig. 1 ) with a Plexiglas spatula.
• Remove the insulation ( 100DL-fig. 1).
• Remove the union ( f-fig. 1).
• Move the ball joint pipe ( g-fig. 1) to gain access to the downstream pipe (u-fig. 1).
(c) Inspect the downstream pipe using a borescope:
• Insert the borescope into the left section of the downstream pipe ( u-fig. 1).
• Check for damage or debris in the left section of the downstream pipe.
• Insert the borescope into the right section of the downstream pipe ( u-fig. 1).
• Check for damage or debris in the right section of the downstream pipe.
(d) Replace the ball joint pipe as follows:
• Put the new pipe in position ( g-fig. 1).
• Connect the pipe ( g-fig. 1) as follow:
• Install the union ( f-fig. 1).
• Install the insulation ( 100DL-fig. 1).
• Apply sealant CAF4 at each end of the insulation (100DL-fig. 1).
• Install the attaching plate:
• Install the clamp ( d-fig. 1) (Refer to TASK 20-41-00-900-809).
• Install the two screws ( c-fig. 1).
• Tighten the screws ( c-fig. 1).
• Connect the exchanger air intake pipe:
• Put the pipe in position ( b-fig. 1).
• Install the nut ( a-fig. 1).
(6) Inspect the brake heating pipes
(a) Remove:
• LH brake heating valve ( L515DL) (Refer to TASK 30-90-01-900-801), FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 7 / 15 DASSAULT AVIATION Proprietary Data
• RH brake heating valve ( R515DL) (fig. 5) (Refer to TASK 30-90-01-900-801).
(b) Inspect the upstream pipe using a borescope:
• Insert the borescope in the pipe ( w-fig. 5).
• Check for damage, nicks or debris.
(c) Inspect the downstream pipe using a borescope:
• Insert the borescope in the pipe ( x-fig. 5).
• Check for damage, nicks or debris.
(d) Check that there is no debris stuck at the end of the brake heating pipe ( y-fig. 5).
(7) Perform a leak chek of the ball joint pipe (Refer to TASK 30-10-00-790-801).
(8) Install all the access doors, fairings and panels.
E. RECORDING Record compliance with this Service Bulletin in the appropriate aircraft documents.
Fill out the card located at the end of the Service Bulletin and mail or fax it to Dassault Aviation or Dassault Falcon Jet, or fill out the electronic Service Bulletin reply form located in the ”Service Bulletin" page on the Falcon portal.
FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 8 / 15 DASSAULT AVIATION Proprietary Data
3. MATERIAL INFORMATION NOTE: Compliance with this Service Bulletin by substituting the part numbers below with interchangeable subsequent part numbers (as per the Master List or Dassault-approved supply list) is acceptable, provided that subsequent part numbers have the same effectivity as the original ones.
A. MODIFICATION KIT Kit P/N SBF2000X0413A Kit P/N SBF2000X0413A
NEW P/N QTY KEY WORD OLD P/N ITEM FIG F2MA724561A2 1 Pipe F2MA724561A2 Refer to (g-fig. 1) B. LOCAL PROCUREMENT
(1) Installation of pipes ( r-fig. 4):
• Seal ( l-fig. 4) P/N W932-24B - qty: 4
• Seal ( n-fig. 4) P/N W932-32B - qty: 4
(2) Installation of the outboard telescopic ducts:
• Seal P/N W932-24B - qty: 4
• O-ring P/N R04095X262A50D7 - qty: 2
(3) Installation of outboard piccolo tubes:
• O-ring ( ad-fig. 3) P/N R04095X262A50D7 - qty: 2
(4) As indicated in the Consumable products manual (CPM):
• sealant CAF4
• lubricant for seals in contact with hot air or liquid soap
• high temperature sealant FALCON 2000 F2000 -441 June 20, 2017 F2000 -30-13 Initial issuance Page 9 / 15 DASSAULT AVIATION Proprietary Data
DASSAULT SERVICE BULLETIN
AVIATION FALCON 2000 F2000 -441 Ball joint Detail A Detail A Detail B Detail C Detail C Detail B Figure 1: REPLACEMENT OF THE BALL JOINT June 20. 2017 F2000-30-13 Initial issuance Page 10 / 15